Dynamic characteristics of a two-stage variable-mass flexible missile with internal flow / Leonard Meirovitch and John Bankovskis.
A general formulation of the dynamical problems associated with powered flight of a two stage flexible, variable-mass missile with internal flow, discrete masses, and aerodynamic forces is presented. The formulation comprises six ordinary differential equations for the rigid body motion, 3n ordinary...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. : Springfield, Va. :
National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor],
1972.
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| Series: | NASA contractor report ;
NASA CR-2076. |
| Subjects: |
MARC
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| 100 | 1 | |a Meirovitch, Leonard. |0 http://id.loc.gov/authorities/names/n83132790 |1 http://isni.org/isni/0000000115606134. | |
| 245 | 1 | 0 | |a Dynamic characteristics of a two-stage variable-mass flexible missile with internal flow / |c Leonard Meirovitch and John Bankovskis. |
| 260 | |a Washington, D.C. : |b National Aeronautics and Space Administration ; |a Springfield, Va. : |b For sale by the National Technical Information Service [distributor], |c 1972. | ||
| 300 | |a iii, 135 pages : |b illustrations ; |c 27 cm. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
| 337 | |a unmediated |b n |2 rdamedia. | ||
| 338 | |a volume |b nc |2 rdacarrier. | ||
| 490 | 1 | |a NASA contractor report, |v NASA CR-2076. | |
| 500 | |a Cover title. | ||
| 500 | |a "June 1972." | ||
| 504 | |a Includes bibliographical references (pages 118-120) | ||
| 520 | |a A general formulation of the dynamical problems associated with powered flight of a two stage flexible, variable-mass missile with internal flow, discrete masses, and aerodynamic forces is presented. The formulation comprises six ordinary differential equations for the rigid body motion, 3n ordinary differential equations for the n discrete masses and three partial differential equations with the appropriate boundary conditions for the elastic motion. This set of equations is modified to represent a single stage flexible, variable-mass missile with internal flow and aerodynamic forces. The rigid-body motion consists then of three translations and three rotations, whereas the elastic motion is defined by one longitudinal and two flexural displacements, the latter about two orthogonal transverse axes. The differential equations are nonlinear and, in addition, they possess time-dependent coefficients due to the mass variation. | ||
| 536 | |a Prepared by University of Cincinnati, Cincinnati, Ohio for Langley Research Center |c NGR 36-004-030. | ||
| 650 | 0 | |a Rockets (Aeronautics) |x Aerodynamics |x Computer simulation. | |
| 650 | 7 | |a Aeroelasticity. |2 nasat. | |
| 650 | 7 | |a Dynamic structural analysis. |2 nasat. | |
| 650 | 7 | |a Missile structures. |2 nasat. | |
| 650 | 7 | |a Residual stress. |2 nasat. | |
| 650 | 7 | |a Flexible bodies. |2 nasat. | |
| 650 | 7 | |a Internal combustion engines. |2 nasat. | |
| 650 | 7 | |a Thrust loads. |2 nasat. | |
| 650 | 7 | |a Transient response. |2 nasat. | |
| 650 | 7 | |a Variable mass systems. |2 nasat. | |
| 700 | 1 | |a Bankovskis, John. | |
| 710 | 2 | |a University of Cincinnati. |0 http://id.loc.gov/authorities/names/n79034519 |1 http://isni.org/isni/0000000121799593. | |
| 710 | 2 | |a Langley Research Center. |0 http://id.loc.gov/authorities/names/n79134855 |1 http://isni.org/isni/0000000406376754. | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://isni.org/isni/0000000449071619. | |
| 776 | 0 | 8 | |i Online version: |a Meirovitch, Leonard. |t Dynamic characteristics of a two-stage variable-mass flexible missile with internal flow. |d Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972 |w (OCoLC)761373385. |
| 830 | 0 | |a NASA contractor report ; |v NASA CR-2076. |0 http://id.loc.gov/authorities/names/n83825229. | |
| 856 | 4 | 2 | |u https://www.hathitrust.org/ |z Search for the full-text version of this title in HathiTrust |
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